Transition reversal and one of its causes
Author:
Affiliation:
1. USSR Academy of Sciences, Novosibirsk, USSR
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7812
Reference24 articles.
1. Experiments on Boundary-Layer Transition at Supersonic Speeds
2. Determination of Distribution of Twist of a Straight Wing to Correspond to the Aerodynamic-Load Distribution on a Sweptback Wing
3. Experiments on Boundary-Layer Transition at Supersonic Speeds
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